{
  "$type": "site.standard.document",
  "description": "A crankcase for a UAV internal combustion engine, comprising a crankcase housing comprising a crankcase chamber, a fuel injection port extending through said crankcase housing to said crankcase chamber, and a fuel diverter comprising a diverting surface disposed within said crankcase chamber and…",
  "path": "/patents/1367216",
  "publishedAt": "2024-07-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02M37/0047",
    "Northwest ULD, Inc. (DBA Northwest UAV)"
  ],
  "textContent": "A crankcase for a UAV internal combustion engine, comprising a crankcase housing comprising a crankcase chamber, a fuel injection port extending through said crankcase housing to said crankcase chamber, and a fuel diverter comprising a diverting surface disposed within said crankcase chamber and aligned with said fuel injection port.",
  "title": "ENGINE WITH DIVERTER FOR HEAVY FUEL INJECTION"
}